EP0246915A1 - Grenzschichtdurchflussregelung - Google Patents

Grenzschichtdurchflussregelung Download PDF

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Publication number
EP0246915A1
EP0246915A1 EP87304578A EP87304578A EP0246915A1 EP 0246915 A1 EP0246915 A1 EP 0246915A1 EP 87304578 A EP87304578 A EP 87304578A EP 87304578 A EP87304578 A EP 87304578A EP 0246915 A1 EP0246915 A1 EP 0246915A1
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EP
European Patent Office
Prior art keywords
projections
riblets
surface according
height
pattern
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP87304578A
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English (en)
French (fr)
Other versions
EP0246915B1 (de
Inventor
Anthony Mark Savill
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
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Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from GB868612486A external-priority patent/GB8612486D0/en
Priority claimed from GB878706554A external-priority patent/GB8706554D0/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of EP0246915A1 publication Critical patent/EP0246915A1/de
Application granted granted Critical
Publication of EP0246915B1 publication Critical patent/EP0246915B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
    • B63B1/34—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/26—Boundary layer controls by using rib lets or hydrophobic surfaces
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T70/00—Maritime or waterways transport
    • Y02T70/10—Measures concerning design or construction of watercraft hulls

Definitions

  • This invention is concerned with the modification of turbulent boundary layer flows over aerodynamic and hydrodynamic surfaces.
  • Walsh's paper reports the investigation of a number of alternative rib profiles and states that he was able to obtain a maximum drag reduction of 7% using V-groove riblets, this representing substantially the greatest reduction of skin friction drag that experimenters have been able to obtain up to the present.
  • the drag reduction may be associated with the ability of the riblets to limit random spanwise movements of the streaks, as has been suggested by a number of sources, e.g. R.E. Falco (AIAA-83-0377, AIAA 21st Aerospace Sciences Meeting, January 10-13 1983, Reno, Nevada). Johansen and Smith (AIAA-85-0547, AIAA-Shear Flow Control Conference, March 12-14, 1985, Boulder, Colorado) have shown that cylindrical riblets of a smaller height than the V-groove riblets with which Walsh obtained his optimum results, have the effect of anchoring and/or creating sites of low-speed streaks in a limited region above the wall surface, but their experiments also showed drag increases of 3% to 8%. More recently, S.P.
  • Wilkinson has attempted to follow Johansen and Smith by using blade riblets to anchor or create low-speed streaks by the use of riblets and then use V-groove riblets between the streak anchors to control bursting, but it is not yet reported whether a net drag reduction has been achieved thereby.
  • riblet surfaces are less susceptible to damage and they can be formed relatively straightforwardly, e.g. by machining or pressing or by the application of a preformed, e.g. extruded layer. It would clearly be preferable to employ such surfaces if they were able to give greater reductions of skin friction drag.
  • an aerodynamic or hydrodynamic wall surface which is provided with a series of elongate projections extending in the direction of fluid flow relative to the surface for modification of a turbulent boundary layer on said surface, said projections being disposed in a repeated spanwise pattern in which the adjacent projections in each pattern repeat project to different heights.
  • the projections preferably form a substantially continuous spanwise array of riblets. It is also preferred to form the projections with sharp-peaked profiles.
  • the repeated pattern consists of alternating higher and lower riblets. It is possible, however, to form a pattern of riblets of three, or even more than three, heights that will provide advantages over the known uniform height riblet surfaces. Such patterns are preferably symmetrical.
  • the lower riblets function to inhibit turbulent eddy motions in the boundary layer from penetrating to all parts of the wall surface, in particular deep into their grooves, resulting in a displacement of the turbulent motion away from the wall with the establishment of a virtual surface some 3/4 of their height above the wall.
  • the alternating higher riblets are so scaled in relation to the lower riblets and the boundary layer thickness that they have the function of extending this effect to its limit; because of their greater scale their action is complementary to that of the lower riblets and the turbulent eddy motions are kept further from the wall surface.
  • riblets of the kind already known function wholly or primarily in a passive manner and do not have any significant influence on the evolution of the eddies themselves. This may also be true of the wall surface configurations of the present invention, but a greater reduction of skin friction can be obtained because, in addition to providing their own contribution the lower riblets modify the deep boundary layer region so that the higher riblets can be similarly operative at a greater distance from the wall surface.
  • the riblets may also have some effect in inhibiting the spanwise gradients associated with the formation of longitudinal vortices or "streaks" in the boundary layer and initiating secondary, smaller-scale longitudinal eddies.
  • this would seem not to be a major effect, and the improvement offered by the present invention does not rely on the riblets having such an influence.
  • the relatively low efficiency of the known riblet surfaces may also be because their performance tends to be self-limiting.
  • the displacement of turbulent eddy motions away from the wall surface by the riblets tends to reduce the wall shear stress, which has a scaling influence reducing the effective height of the riblets, and therefore curbing their efficiency.
  • the higher riblets are present to reinforce the action of the lower riblets and so force the turbulent eddy motions further from the wall surface. At the same time this automatically compensates for any loss of efficiency of the smaller riblets.
  • Another secondary benefit is also obtainable because there is some degree of progressive reduction of with the stream development length (i.e. the streamwise distance along the wall surface) that may be significant in the transition region and the early part of the turbulent boundary layer.
  • the smaller riblets of a suitable height for an early region of the turbulent boundary layer will therefore progressively show less effect along their length, but the higher riblets now present extend the effective area of the ribbing to a greater stream development length.
  • At least the higher riblets have side faces that are inclined at an angle that varies over the height of the projections, each said side face having an intermediate region at a lesser steepness than the adjacent regions above and below said region and forming the lower part of a concave profile peak of the associated projection.
  • the pattern of projections consists of alternating higher and lower projections
  • smaller and higher projections can be arranged to displace turbulent eddy motions in the boundary layer away from the wall surface.
  • the higher projection can be so scaled in relation to the smaller projections that they have the function of extending this effect to its limit.
  • the transition to the concave-sided peaks should be positioned at or close to the virtual wall height established by the projections.
  • the region below the transition preferably has substantially planar faces so as to form a series of steep-sided V-grooves between the projections in their lowest reaches. These can act in the manner already described to displace the turbulent motion away from the wall surface.
  • the longitudinal vortices displaced above the virtual wall surface are then controlled by the concave peaks projecting into this region which, by virtue of their different profile, can act more strongly on the vortices. If the enhanced displacement of the virtual wall surface resulting from the combination of projection heights puts that virtual surface above the height of the smallest projections, no benefit is achieved by modifying their side faces.
  • any of the smaller projections extends above the virtual wall position, it is an advantage that their side faces be given a varied inclination similarly, with the transition substantially at the height of the virtual wall position. This may result in a change of inclination occurring at a particular height above the actual wall surface that is the origin of the projections, but in particular cases the pattern of projections may produce a virtual wall surface height that varies spanwise with the projection pattern, and the positions of the changes of inclination on the individual projections can then follow those changes of height.
  • the transition to the concave profile may be substantially sharp-­edged, but it is also possible to have a radiussed or chamfered transition.
  • the concave faces are preferably continuously curved to a relatively sharp-edged tip but it is also possible to build them up from a group of straight and/or curved sections and for convenience the tip itself may be flattened or radiussed.
  • the wall surface is shown with alternating higher riblets R and lower riblets r, this pattern being repeated spanwise and the riblets running in the stream direction over the surface in the turbulent boundary layer region, and preferably starting from the transition region of the flow over the surface.
  • the pattern extending streamwise preferably continues over all the turbulent boundary layer area of the surface. It is not essential that the riblets be aligned precisely with the fluid stream and deviations of up to 10°-15° can be tolerated.
  • the riblets are all shown with triangular profiles, but other profiles can be used, another preferred profile having a sharp-peaked from (apex included angle preferably not greater than about 20°) with concave valleys between successive peaks, as is illustrated with the riblets R ⁇ , r ⁇ in Fig. 2. Triangular riblets separated by narrow flat valleys can also be used. Furthermore, while Fig. 1 shows both the large and small riblets with the same base widths to give relatively sharp isosceles triangular profiles, it may be preferred to increase the base widths to about twice the heights of the respective riblets; this is particularly relevant to cusp-shaped profiles shown in Fig. 2.
  • the preferred sizes and dimensional relationships of the riblets may be expressed in the non-dimensional form of so-called "law of the wall” variables in which actual distance values are multiplied by a "wall unit” scalar quantity defined as: where ⁇ is the wall shear stress, ⁇ is the fluid density, and ⁇ is the fluid kinematic viscosity.
  • the smaller riblets r have a non-dimensionalised height h+ of 15 units and larger riblets R have a height h L of 25 units.
  • the width w+ of each of the riblets is 7.5 units giving a pitch s L + of 15 units for the pattern repeat.
  • a virtual surface is established for the turbulent boundary layer flow above the wall surface itself.
  • the influence of the riblets r may be sufficient to set this virtual surface some three-quarters of their height above the wall surface, so that the effective height (h le +) of the larger riblets R, i.e. their height above the virtual surface, is therefore approximately 13 units, but the larger riblets add their own influence in the region above this so that the virtual surface is displaced further out.
  • the ratio h:s is preferably not substantially less than 1:2 nor substantially greater than 2:1. Within this range the aspect ratio (height:base width) can be higher especially for the large riblets.
  • the preferred size ranges in non-dimensional wall units for low speed flow for the smaller riblets r, 2 ⁇ h+ ⁇ 20; preferably 5 ⁇ h+ ⁇ 15 for the larger riblets R, 8 ⁇ h le + ⁇ 45; preferably 15 ⁇ h le + ⁇ 35 for the pattern repeat pitch, 6 ⁇ s l + ⁇ 50; preferably 20 ⁇ s l + ⁇ 40.
  • the pattern repeat pitch will be increased while maintaining substantially the same base widths for the individual riblets.
  • riblets of three different heights i.e. riblets r i of an intermediate height being interposed between higher and lower riblets in the manner illustrated in Fig. 3
  • the pattern repeat pitch is doubled. This is also the case for the example shown in Fig. 4 where the heights of the riblets decrease to a minimum in a region centrally positioned between the higher riblets.
  • the profiles of the different height riblets may be different.
  • Figs. 5 to 7 illustrate further wall surface riblet patterns within the scope of the invention and having modified riblet profiles.
  • a virtual wall surface is established at 3 ⁇ 4 the height of the smaller riblets r in a pattern of alternating riblets of two different heights.
  • the pattern pitch is 15 wall units, which is therefore the pitch (s+, s l +) of both the smaller and larger riblets.
  • the height of the smaller riblets is 15 wall units and that of the higher riblets R is 25 wall units; above the virtual wall surface they have a height (h le +) 13 units for the larger riblets and (h e +) 3 units for the smaller riblets. From the point of transition t the side faces of the riblets extend upwards with the sharp-­peaked concave profiles already described while below the virtual wall surface they form deep-sided V-grooves.
  • Fig. 6 illustrates a modification of the example in Fig. 5 in which this occurs and it shows that in addition to the 3 ⁇ 4h+ displacement of the wall surface produced by the smaller riblets, the larger riblets may induce a further displacement of 3 ⁇ 4h le + so that the virtual wall surface is at a height of approximately (3 ⁇ 4h+ + 3 ⁇ 4h le +).
  • the height of the smaller riblets being less than this they therefore have a completely planar profile, while side faces of the larger riblets are given their concave form over their effective height (h lE +) from the raised virtual wall surface.
  • a riblet pattern in which the height changes between successive riblets produces a similarly undulating virtual wall surface, especially if the pattern consists of more than two riblets.
  • This can be accommodated by a configuration such as is shown in Fig. 7.
  • the virtual wall surface height for the smaller riblets r corresponds to that in the example of Fig. 5, whereas for the larger riblets R it corresponds to that in Fig. 6.
  • the point of inflection of the smaller riblets, i.e. their intersection with the virtual surface is at 3 ⁇ 4h+ above the real surface, i.e.
  • the point of inflection is at approximately (3 ⁇ 4h+ + 3 ⁇ 4h le +) above the real surface.
  • the portion of the smaller riblets having a concave profile thus extends over a height 1 ⁇ 4h l + while the concave profile of the larger riblets extends over a height 1 ⁇ 4(h l + - 3 ⁇ 4h+).
  • FIG. 9 illustrates how, with a spanwise pattern of riblets r1, r2 of two different heights, the smaller riblets r1 can be succeeded by a third series of riblets r3 higher than the previously larger riblets r2, and if a further stage is required the latter can be succeeded by a fourth still larger series, so that at each station in the direction of the stream the pattern is always composed of riblets o two different heights.
  • Fig. 9 also indicates at r L how, at the leading edge of the riblet pattern the riblets can be faired into the wall surface to avoid a drag increase due to the flow meeting a bluff leading face. When there is a progressive stepped increase of the height of the riblets, as described above, the leading edge of each step may be faired similarly, although this is not illustrated.
  • the invention is generally applicable to the wall surfaces of bodies in which a reduction of skin friction is sought. It may thus provide a means of reducing drag on the external surfaces of vehicles, including aircraft, land vehicles and watercraft. It can also be used in machines, e.g. the blading, both rotating and stationary, of turbo-­machines, and for the internal surfaces of pipes and conduits. It will be understood that the invention includes the possibilities of forming the surface projections integrally with the bodies concerned and also of providing surface elements, e.g. as sheets or tapes, having the projections, for application to bodies to provide the required surface configurations thereon.

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)
EP87304578A 1986-05-22 1987-05-22 Grenzschichtdurchflussregelung Expired - Lifetime EP0246915B1 (de)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB868612486A GB8612486D0 (en) 1986-05-22 1986-05-22 Control of boundary layer flow
GB8612486 1986-05-22
GB878706554A GB8706554D0 (en) 1987-03-19 1987-03-19 Boundary layer devices
GB8706554 1987-03-19

Publications (2)

Publication Number Publication Date
EP0246915A1 true EP0246915A1 (de) 1987-11-25
EP0246915B1 EP0246915B1 (de) 1991-08-28

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EP87304578A Expired - Lifetime EP0246915B1 (de) 1986-05-22 1987-05-22 Grenzschichtdurchflussregelung

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EP (1) EP0246915B1 (de)
DE (1) DE3772448D1 (de)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0284187A1 (de) * 1987-03-19 1988-09-28 ROLLS-ROYCE plc Grenzschichteinrichtungen
GB2210011A (en) * 1987-09-16 1989-06-01 Francis John Mcvey Aerodynamic covering
WO1995011388A1 (de) * 1993-10-20 1995-04-27 Josef Moser Oberfläche eines fluidumströmten körpers
WO2003087604A1 (de) * 2002-04-17 2003-10-23 Röhm GmbH & Co. KG Festkörper mit mikrostrukturierter oberfläche
AT500159B1 (de) * 2001-10-01 2006-06-15 Atomic Austria Gmbh Schi, sprungschi oder snowboard mit einer strukturierten oberfläche
US11618511B2 (en) 2021-01-12 2023-04-04 Honda Motor Co., Ltd. Surface pattern for a vehicle

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0205289A1 (de) * 1985-05-31 1986-12-17 Minnesota Mining And Manufacturing Company Einrichtung zur Verringerung des Luftwiderstandes
EP0216384A2 (de) * 1985-09-26 1987-04-01 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Einrichtung zur Verringerung des Reibungswiderstandes

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0205289A1 (de) * 1985-05-31 1986-12-17 Minnesota Mining And Manufacturing Company Einrichtung zur Verringerung des Luftwiderstandes
EP0216384A2 (de) * 1985-09-26 1987-04-01 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Einrichtung zur Verringerung des Reibungswiderstandes

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
AIAA'83 - AIAA 21st AEROSPACE SCIENCES MEETING, Reno, Nevada, 10th-13th January 1983, pages 6,18, American Institute of Aeronautics and Astronautics, New York, US; D.M. BUSHNELL: "AIAA-83-0227 - Turbulent drag reduction for external flows" *
MECHANICAL ENGINEERING, vol. 103, no. 3, March 1981, page 71, New York, US; "Grooves reduce aircraft drag" *

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0284187A1 (de) * 1987-03-19 1988-09-28 ROLLS-ROYCE plc Grenzschichteinrichtungen
GB2210011A (en) * 1987-09-16 1989-06-01 Francis John Mcvey Aerodynamic covering
WO1995011388A1 (de) * 1993-10-20 1995-04-27 Josef Moser Oberfläche eines fluidumströmten körpers
US5860626A (en) * 1993-10-20 1999-01-19 Moser; Josef Surface of a body exposed to circumfluent fluid
AT500159B1 (de) * 2001-10-01 2006-06-15 Atomic Austria Gmbh Schi, sprungschi oder snowboard mit einer strukturierten oberfläche
WO2003087604A1 (de) * 2002-04-17 2003-10-23 Röhm GmbH & Co. KG Festkörper mit mikrostrukturierter oberfläche
US7041363B2 (en) 2002-04-17 2006-05-09 Roehm Gmbh & Co. Kg Solid body with microstructured surface
US11618511B2 (en) 2021-01-12 2023-04-04 Honda Motor Co., Ltd. Surface pattern for a vehicle

Also Published As

Publication number Publication date
DE3772448D1 (de) 1991-10-02
EP0246915B1 (de) 1991-08-28

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